ES2266996T3 - Dispositivo de colgamiento de un turbo-propulsor bajo un plano de sustentacion de una aeronave. - Google Patents

Dispositivo de colgamiento de un turbo-propulsor bajo un plano de sustentacion de una aeronave. Download PDF

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Publication number
ES2266996T3
ES2266996T3 ES04106154T ES04106154T ES2266996T3 ES 2266996 T3 ES2266996 T3 ES 2266996T3 ES 04106154 T ES04106154 T ES 04106154T ES 04106154 T ES04106154 T ES 04106154T ES 2266996 T3 ES2266996 T3 ES 2266996T3
Authority
ES
Spain
Prior art keywords
rigid
drawer
turbo
hanging
section
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
ES04106154T
Other languages
English (en)
Spanish (es)
Inventor
Stephane Machado
Jerome Cassagne
Anthony Del Blanco
Yvon Martin
Arnaud Chambreuil
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Application granted granted Critical
Publication of ES2266996T3 publication Critical patent/ES2266996T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Body Structure For Vehicles (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Vibration Prevention Devices (AREA)
ES04106154T 2003-12-01 2004-11-29 Dispositivo de colgamiento de un turbo-propulsor bajo un plano de sustentacion de una aeronave. Expired - Lifetime ES2266996T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0350946A FR2862944B1 (fr) 2003-12-01 2003-12-01 Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
FR0350946 2003-12-01

Publications (1)

Publication Number Publication Date
ES2266996T3 true ES2266996T3 (es) 2007-03-01

Family

ID=34451760

Family Applications (1)

Application Number Title Priority Date Filing Date
ES04106154T Expired - Lifetime ES2266996T3 (es) 2003-12-01 2004-11-29 Dispositivo de colgamiento de un turbo-propulsor bajo un plano de sustentacion de una aeronave.

Country Status (7)

Country Link
US (1) US7159819B2 (fr)
EP (1) EP1538080B1 (fr)
AT (1) ATE330844T1 (fr)
CA (1) CA2487841C (fr)
DE (1) DE602004001319T2 (fr)
ES (1) ES2266996T3 (fr)
FR (1) FR2862944B1 (fr)

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* Cited by examiner, † Cited by third party
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FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
FR2870821B1 (fr) * 2004-05-25 2007-08-17 Airbus France Sas Aeronef comprenant un dispositif de detection et/ou de mesure de perturbations atmospheriques
US20060145001A1 (en) * 2004-12-30 2006-07-06 Smith Matthew C Fan cowl door elimination
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2887851B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891252B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Mat a ossature monolithique
FR2891526B1 (fr) * 2005-10-03 2007-11-02 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
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FR2915178B1 (fr) * 2007-04-23 2009-07-10 Airbus France Sa Attache d'un caisson de mat sur une voilure, pincant un panneau lateral du caisson
FR2916736B1 (fr) * 2007-06-04 2009-09-04 Airbus France Sa Dispositif d'accrochage d'un turbopropulseur d'aeronef comprenant des moyens de fixation hydrauliques.
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FR2934845A1 (fr) * 2008-08-11 2010-02-12 Airbus France Mat de moteur pour aeronef
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FR2976914B1 (fr) * 2011-06-23 2014-12-26 Snecma Structure d'accrochage d'une turbomachine
FR3005033B1 (fr) * 2013-04-26 2015-05-15 Snecma Structure de suspension d'un turbopropulseur a double helices non carenees sur un element structurel d'un aeronef
JP6266775B2 (ja) 2013-07-26 2018-01-24 エムアールエイ・システムズ・エルエルシー 航空機エンジンパイロン
EP3071481B1 (fr) 2013-11-18 2020-01-08 LORD Corporation Systèmes et procédés de fixation d'un groupe motopropulseur
FR3013678B1 (fr) * 2013-11-25 2015-11-20 Airbus Operations Sas Carenage aerodynamique
FR3016344B1 (fr) * 2014-01-10 2017-09-01 Snecma Structure de suspension d'un turbopropulseur a double helices non carenees sur un element structurel d'un aeronef a fixation rigide de la structure d'entree d'air
US9238511B2 (en) * 2014-03-04 2016-01-19 Mra Systems, Inc. Engine pylon structure
FR3054202B1 (fr) * 2016-07-25 2018-07-13 Safran Aircraft Engines Berceau pour turbopropulseur a manche d'entree d'air integree
FR3058704B1 (fr) * 2016-11-14 2018-11-16 Safran Aircraft Engines Berceau bipartite a coulissement pour turbopropulseur
FR3071820B1 (fr) * 2017-10-03 2020-12-04 Airbus Operations Sas Ensemble moteur d'aeronef
FR3072945B1 (fr) * 2017-10-27 2020-11-20 Airbus Operations Sas Structure primaire de mat de support d'un groupe propulseur d'aeronef comportant une partie inferieure en u obtenue de maniere monobloc ou par soudage
FR3079215B1 (fr) * 2018-03-22 2020-11-20 Airbus Operations Sas Carenage avant d'un mat d'aeronef comprenant une coiffe mobile et aeronef equipe dudit carenage avant
US11635024B2 (en) 2019-08-16 2023-04-25 Pratt & Whitney Canada Corp. Pusher turboprop powerplant installation
US11674414B2 (en) * 2021-03-19 2023-06-13 Pratt & Whitney Canada Corp. Gas turbine engine and mount assembly therefor
US12415610B2 (en) * 2022-05-13 2025-09-16 The Boeing Company Strut assembly and method for coupling an engine to a wing of an aircraft
CN116119023B (zh) * 2023-04-17 2023-07-18 成都沃飞天驭科技有限公司 飞行器测试平台及其主框架、主框架的设计方法
EP4488181A1 (fr) * 2023-07-06 2025-01-08 Airbus Operations (S.A.S.) Système de propulsion pour aéronef comprenant un turboréacteur, un mât et une attache moteur
FR3164697A1 (fr) * 2024-07-19 2026-01-23 Airbus Operations (S.A.S.) Mât réacteur comportant une structure primaire et une structure secondaire avant avec des moyens de fixation de l’une à l’autre

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US4437627A (en) * 1982-03-12 1984-03-20 The Boeing Company Integrated power plant installation system
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US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
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US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
FR2793768B1 (fr) * 1999-05-17 2001-09-07 Aerospatiale Airbus Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif
US6330985B1 (en) * 2000-06-30 2001-12-18 General Electric Company Link component for aircraft engine mounting systems
GB2375513B (en) * 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
FR2830516B1 (fr) * 2001-10-04 2004-01-02 Snecma Moteurs Suspension de turboreacteur
FR2851226B1 (fr) * 2003-02-19 2005-05-20 Snecma Moteurs Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse
FR2862612B1 (fr) * 2003-11-25 2006-02-17 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
FR2862611B1 (fr) * 2003-11-25 2007-03-09 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
FR2862610B1 (fr) * 2003-11-25 2007-03-23 Airbus France Dispositif d'accrochage reliant un moteur et une voilure d'aeronef
FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
FR2862945B1 (fr) * 2003-12-01 2006-04-28 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef.
US7104306B2 (en) * 2004-06-14 2006-09-12 The Boeing Company Cast unitized primary truss structure and method

Also Published As

Publication number Publication date
EP1538080A1 (fr) 2005-06-08
US7159819B2 (en) 2007-01-09
US20050116093A1 (en) 2005-06-02
DE602004001319D1 (de) 2006-08-03
FR2862944B1 (fr) 2006-02-24
CA2487841A1 (fr) 2005-06-01
FR2862944A1 (fr) 2005-06-03
ATE330844T1 (de) 2006-07-15
DE602004001319T2 (de) 2007-06-14
CA2487841C (fr) 2012-09-18
EP1538080B1 (fr) 2006-06-21

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